J-GLOBAL ID:201110050903216423   Research Resource code:5000003252 Update date:Nov. 01, 2004

0.5m Hypersonic Wind Tunnel

Owning Organization:
Contact: HAMAMOTO Shigeru
Resource classification: Experience equipment, Facilities, etc
Hypersonic wind tunnel with 50 cm of diameter of nozzle
exit. Mach number of 5, 7, 9 and 11. (replaceable nozzle)
Constructed in 1965
Type: Intermittent blow-down type (Vacuum suction is
Use: Aerodynamic research at hypersonic speed, and
development test for supersonic plane and flying object
User procedures and method:
Refer to Web Page of JAXA.

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